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This image is part of a series that was created for an open textbook, Aerodynamics and Aircraft Performance. The textbook is available here.
Kindred Grey (2021). "Finding the Center of Pressure." CC BY 4.0. Adapted from James F. Marchman (2004). CC BY 4.0.
Alternative text:
A curved line representing cambered airfoil is divided into 9 equal segments, with each having a corresponding cap Gamma at their quarter chord. A point, cap X sub c p, is shown at the quarter chord of the straight line connecting the leading and trailing edges.
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